How to Calculate Flight Speed given Thrust in Turbojet?
Flight Speed given Thrust in Turbojet calculator uses Flight Speed = Exit Velocity-(Net Thrust of Turbojet-Nozzle Exit Area*(Nozzle Exit Pressure-Ambient Pressure))/(Mass Flow Rate Turbojet*(1+Fuel Air Ratio)) to calculate the Flight Speed, Flight Speed given Thrust in Turbojet formula is defined as speed of flight after considering expansion velocity and gross thrust produced by turbojet engine. Flight Speed is denoted by V symbol.
How to calculate Flight Speed given Thrust in Turbojet using this online calculator? To use this online calculator for Flight Speed given Thrust in Turbojet, enter Exit Velocity (Ve), Net Thrust of Turbojet (T), Nozzle Exit Area (Ae), Nozzle Exit Pressure (pe), Ambient Pressure (p∞), Mass Flow Rate Turbojet (ma) & Fuel Air Ratio (f) and hit the calculate button. Here is how the Flight Speed given Thrust in Turbojet calculation can be explained with given input values -> 130.2403 = 213-(469-0.0589*(982-101))/(5*(1+0.008)).